1EFF : ALL 1 27-84-63Page 435 1 1 May 01/05R 1 1 1CES 1
(15) Fully tighten the screws (51) and (54).
**ON A/C 001-049, 051-061, 101-105, 201-203,
Subtask 27-84-63-420-053
E. Connection of the Slat-To-Track Bonding Strap
(Ref. Fig. 402/TASK 27-84-63-991-002)
(1) Attach the bonding strap (2) with the bolt (8) and the nut (1) (Ref. TASK 20-28-00-912-004).
(2) Safety the bolts (8) with MISCELLANEOUS (Material No. 19-010). R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
Subtask 27-84-63-420-053-A
E. Connection of the Slat-To-Track Bonding Strap (Track 1)
(Ref. Fig. 402A/TASK 27-84-63-991-002-A)
(1) Attach the bonding strap (2) with the bolt (8) and the nut (1) (Ref. TASK 20-28-00-912-004).
(a) Safety the bolts (8) with MISCELLANEOUS (Material No. 19-010). **ON A/C ALL
Subtask 27-84-63-860-052
F. Aircraft Maintenance Configuration
(1)
Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) (98D27804001000) to manually retract the slats to the zero position.
(2)
Energize the ground service network
(Ref. TASK 24-42-00-861-001).
(3)
On the MCDU display, make sure that the PPU DATA page is shown (to monitor the slats PPU position).
(4)
If necessary, use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to move the slat drive shaft until the PPU data shows the same values as recorded in Para. 3.B.:
-
the FPPU angle value must agree +/- 0.1 deg.
-
the APPU angle value must agree +/- 0.1 deg.
-
the FPPU and APPU angles must agree +/- 1.3 deg.
-
the LH APPU and the RH APPU angles must agree +/- 0.45 deg.
(5)
De-energize the ground service network
(Ref. TASK 24-42-00-862-001).
(6)
Remove the ADAPTOR-DRIVE, SLAT (AND FLAP) and the pneumatic wrench from the slat drive shaft.
(7)
Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT, installed outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 27-50-00-000-003).
Subtask 27-84-63-865-054
G. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV, 9CV, 11CV.
Subtask 27-84-63-410-053
H. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the safety collar on the circuit breakers 9CV and 11CV.
(3)
Install the applicable torque shaft (Ref. TASK 27-84-45-400-005):
-
for the left wing, install FIN 6010CM
-
for the right wing, install FIN 6060CM.
(4)
Install the applicable access panel (Ref. TASK 57-41-37-400-006):
-
for the left wing, install 522NB
-
for the right wing, install 622NB.
Subtask 27-84-63-220-052
J. Check
(1) Do a check of the permitted aerodynamic tolerances between the slats 1 thru 5 (Ref. TASK 27-80-00-200-002).
Subtask 27-84-63-710-051
K. Test
(1) The operational test of the slat system (Ref. TASK 27-84-00-710-001), was done during the installation of the torque shaft FIN 6010CM (6060CM).
5. Close-up
________ Subtask 27-84-63-942-053
A. Removal of Equipment
(1)
Remove ths safety barriers.
(2)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the slat/flap control lever on panel 114VU.
(3)
Remove the warning notice(s).
(4)
Remove the access platform(s).
(5)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
SLAT 2 - REMOVAL/INSTALLATION_____________________________
TASK 27-84-64-000-001
Removal of the No. 2 Slat
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU_______ START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING_______ GEAR.
R R R WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR._______ MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
1. Reason for the Job__________________
Self Explanatory
2. Job Set-up Information______________________
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱8(124)
